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#31
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| The HP aircraft took a lot of development and even then only really became feasible when technology gave them the materials needed (like Tedlar for the wing skins, etched alloy tapered tubes for the spars, expanded polystyrene for the wing ribs). For centuries people had dreamt of human powered flight, or even tried to build machines, but it wasn't until we developed materials, and a better understanding of aerodynamics, that these things became a reality. HP aircraft still took years of development to get to the point where we can build one pretty easily, with pretty much off-the-shelf materials. If anything, they've got bigger, because the advent of things like stiff and light carbon fibre spars has allowed a bigger span than the tapered, etched alloy spars that the Gossamer series used at first. Same goes for prop design, although the Wrights did pretty well - there props on the Flyer were around 80%, which is better than those on most aircraft flying today. HP aircraft have pushed the prop efficiency boundary up to around 90%, which is probably pretty close to the theoretical maximum (you can never get 100%, because a prop blade will always have some drag). |
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#32
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| It is worth noting, from a practical point of view, that MacCready's HP aircraft, as Jeremy says, didn't pursue ground effect exhaustively. Both Gossamer Condor and Gossamer Albatross were high wing designs. With Gossamer Albatross, the cross channel HPA, There is a recognition that drag caused by turbulence close to the water/wave surface was significant, and that Bryan Allen, the pilot, found the pedaling easier with a little more altitude. Morton Grosser's detailed book, Gossamer Odyssey, is on Google books. ![]() |
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#33
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| I should note that the turbulence issue is associated in particular with the very low power levels available, and is likely to be a much less significant issue with wind power. |
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#34
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| With both aircraft, incidentally, MacCready was achieving wing spans of nearly 30m with unladen weights of only 31, 32 kgs, more than 30 years ago now. |
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#35
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| There's an interesting video here: http://www.youtube.com/watch?v=F4zEaYl01Uw of a NASA concept for a dynamic soaring platform using wind gradients on the ocean surface (above waves / between troughs) modelled on albatross flight. Incidentally, dynamic soaring by sailplane has now been measured at an incredible 468mph. |
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#36
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| Quote:
Here a very detailed article: http://www.howfliesthealbatross.com/...%20Soaring.pdf Using updrafts and downdrafts is usually not called "dynamic soaring" but "static soaring": http://en.wikipedia.org/wiki/Dynamic_soaring Quote:
Quote:
Quote:
http://en.wikipedia.org/wiki/Wind_gradient A free flying vehicle (on constant course and altitude) could (at least theoretically) exploit the velocity difference between the airmass layers, just like a sailboat exploits the velocity difference between air and water. You could use a sail on a ground effect glider (acting as the keel in the slow air) and then a kite in the fast air (acting as the sail). Or use two kites at different altitudes. But it would have to be super efficient to actually work. |
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#37
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| The wind gradient from surface up would be tough to exploit. With wind over water, it only takes a small surface below the water (dagger board) to allow you to create forward thrust from a large sail area. This is with a pretty good velocity difference between adjacent mediums. The wind gradient you seem to be wanting to exploit is a thin region of air close to the surface being one region and the air a good ways up would be the other region. The most efficient way to extract energy from air is a sail or fixed wing as compared to a propeller. The surface area needed to get any real forward thrust would need to be pretty large vertical surfaces for both an upper and a lower. It would also only offer a decent speed differential when the true wind speed is quite high. To get a large surface area in the thin layer close to the surface, the aspect ratio would be very not good. The combined weight of the two vertical wing/sail surfaces would be much higher than the sail / dagger board combination and the forward thrust would be lower. If you want to "fly" using wind your choices are limited. Here are a few items that come to mind in the context of flying sailboats.
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#38
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| Quote:
I was trying to keep the answer brief, but did mention the vertical movement and velocity change needed. |
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